| 编队飞行卫星群的轨道动力学特性与构形设计 |
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| 引用本文： | 肖业伦,张晓敏.编队飞行卫星群的轨道动力学特性与构形设计[J].宇航学报,2001,22(4):7-12. |
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| 作者姓名： | 肖业伦 张晓敏 |
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| 作者单位： | 北京航空航天大学宇航学院, |
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| 基金项目： | 国家自然科学基金资助项目(10082001) |
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| 摘 要： | 编队飞行卫星群由一些相对距离近的小卫星组成,在严格的条件下,若干颗伴随卫星环绕一颗中心卫星作相对运动,相对轨道为特别性质的椭圆,本文研究了编队飞行卫星群的轨道动力学特性,提出了编队飞行的轨道构形设计的原则和方法。
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| 关 键 词： | 编队飞行卫星群 轨道动力学 轨道设计 特性 构形设计 |
| 文章编号： | 1000-1328(2001)04-0007-06 |
ORBITAL DYNAMICAL CHARACTERISTICS AND CONFIGURATION DESIGN OF FORMATION FLYING SATELLITES |
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| Xiao,Yelun,Zhang,Xiaomin.ORBITAL DYNAMICAL CHARACTERISTICS AND CONFIGURATION DESIGN OF FORMATION FLYING SATELLITES[J].Journal of Astronautics,2001,22(4):7-12. |
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| Authors: | Xiao Yelun Zhang Xiaomin |
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| Abstract: | Cluster of formation flying satellites consists of several companion satellites that make relative motion to a central satellite under strict conditions.The trajectory of relative motion is ellipse with special properties.This paper reveals the dynamical characteristics of relative orbital motion of formation flight and presents the principles and method for the orbit configuration design of formation flight. |
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| Keywords: | Formation flying satellites Orbit dynamics Orbit design |
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